A patrol drone
By designing adjustment and buffer components on the patrol drone, the problem of fixed camera angle was solved, enabling flexible camera adjustment and landing protection, thereby improving the comprehensiveness of data collection and the stability of the drone.
Patent Information
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- SHANXI DIAOPU TECH CO LTD
- Filing Date
- 2025-06-23
- Publication Date
- 2026-05-26
AI Technical Summary
Traditional patrol drones have fixed camera angles that cannot be flexibly adjusted according to actual needs, resulting in a limited field of view, inability to fully cover the patrol area or omission of details in key locations, and incomplete or inaccurate data collection.
A patrol drone was designed, employing adjustment and buffer components. The camera angle is adjusted by the cooperation of a motor-driven sliding column and a rotating block, and the buffer component reduces the damage to the fuselage during landing.
It enables flexible adjustment of the camera angle, ensuring comprehensive and accurate data collection, while protecting the drone fuselage when landing in harsh environments, thus improving patrol efficiency and stability.
Smart Images

Figure CN224277598U_ABST
Abstract
Description
Technical Field
[0001] This utility model relates to the field of geological disaster prevention and control, and in particular to a patrol drone. Background Technology
[0002] In the modern intelligent inspection equipment system, the design and application of inspection drones are particularly crucial in the field of geological disaster prevention and control. Among them, the fault prevention function plays a vital role in the stability and operational efficiency of the equipment. Geological disasters are characterized by their suddenness, complexity, and unpredictability. As the core equipment for efficient operation in this field, the operational stability, operational efficiency, and anti-interference capabilities of inspection drones directly affect the effectiveness of geological disaster prevention and control inspection work and the quality of related tasks.
[0003] Patrol drones typically consist of three parts: a flight system, sensor equipment, and a support structure. The flight system's main function is to achieve stable flight in complex terrain through efficient power units and intelligent control algorithms, ensuring the efficiency and safety of patrol missions, especially in adverse weather conditions or challenging tasks, guaranteeing the drone's stable execution. The sensor equipment, as the core component, integrates various high-precision sensors and monitoring technologies. The support structure provides a robust fuselage design, ensuring the drone is unaffected by external interference during flight and capable of supporting the complex sensor equipment, ensuring its long-term stable operation.
[0004] Traditional drones used for geological disaster prevention and control patrols have fixed camera angles, which cannot be flexibly adjusted according to actual patrol needs. This limits the field of view, resulting in incomplete coverage of the patrol area or omission of details in certain key locations. If the flight altitude or angle changes, the fixed-angle camera may not be able to effectively capture the target object, leading to incomplete or inaccurate data collection. Therefore, a patrol drone is proposed to solve the above problems. Utility Model Content
[0005] To overcome the above shortcomings, this utility model provides a patrol drone, which aims to improve the problem of camera angle locking during patrol in existing drones.
[0006] To achieve the above objectives, the present invention adopts the following technical solution:
[0007] A patrol drone includes a fuselage, an adjustment component fixedly connected to the outside of the fuselage, and a buffer component fixedly connected to the outside of the fuselage;
[0008] The adjustment assembly includes a rotating ball, two rotating blocks are fixedly and slidably connected to the outside of the rotating ball, one of the rotating blocks is fixedly and slidably connected to a sliding shaft, a lower sliding column is slidably connected to the outside of the sliding shaft, an upper sliding column is slidably connected to the outside of the sliding shaft, the outside of the lower sliding column is in contact with the outside of the upper sliding column, a second motor is fixedly connected to the outside of the lower sliding column, a first motor is fixedly connected to the outside of the upper sliding column, and a first connecting plate is fixedly connected to the outside of the first motor.
[0009] As a further description of the above technical solution:
[0010] The buffer assembly includes a support plate, two connecting blocks II are fixedly connected to the outside of the support plate, a rotating plate is rotatably connected to the outside of the connecting blocks II, a sliding block is rotatably connected to the outside of the rotating plate, a sliding shaft II is slidably connected to the outside of the sliding block, a spring is fixedly connected to the outside of the sliding shaft II, and a connecting plate II is fixedly connected to the outside of the sliding shaft II.
[0011] As a further description of the above technical solution:
[0012] The lower sliding column is fixedly connected to a connecting column one, the upper sliding column is fixedly connected to the outside of the connecting column one, and the connecting column one is fixedly connected to the outside of the connecting plate one.
[0013] As a further description of the above technical solution:
[0014] Another rotating block is externally fixedly connected to a sliding disk, which is fixedly connected to the outside of the first connecting plate;
[0015] As a further description of the above technical solution:
[0016] A connecting block is fixedly connected to the outside of the sliding shaft, and a camera is fixedly connected to the outside of the connecting block.
[0017] As a further description of the above technical solution:
[0018] A buffer column is fixedly connected to the outside of the connecting plate 2, and a connecting column 2 is slidably connected to the outside of the buffer column;
[0019] As a further description of the above technical solution:
[0020] A buffer block is fixedly connected to the outside of the buffer column, and a bracket is fixedly connected to the outside of the buffer block.
[0021] As a further description of the above technical solution:
[0022] Multiple wings are fixedly connected to the outside of the fuselage, and the fuselage is fixedly connected to the outside of the connecting plate.
[0023] This utility model has the following beneficial effects:
[0024] 1. In this utility model, when motor one starts, it drives the upper sliding column to move; when motor two starts, it drives the lower sliding column to move; the upper and lower sliding columns drive the sliding shaft one to move; the sliding shaft one drives the connecting block one to move; the connecting block one drives the camera to move; the sliding shaft one rotates on the rotating ball by the rotating block; and the rotating ball moves on the sliding disk by the rotating block. This solves the problem of camera angle locking during drone patrols.
[0025] 2. In this utility model, when the drone lands, the buffer column is pushed by the buffer block, the buffer column drives the connecting plate two to move, the connecting plate two drives the sliding block to slide on the sliding shaft, so the rotating plate is driven by the sliding block, and the connecting block two provides support to the rotating plate. Therefore, the spring is compressed, buffering the energy generated by the fall, thus solving the problem that the drone is easily damaged when landing due to the harsh patrol environment. Attached Figure Description
[0026] Figure 1 This is a three-dimensional schematic diagram of the fuselage of a patrol drone proposed in this utility model;
[0027] Figure 2 This is a schematic diagram of the structure of a connecting plate for a patrol drone proposed in this utility model;
[0028] Figure 3 This is a schematic diagram of the rotating ball structure of a patrol drone proposed in this utility model;
[0029] Figure 4 for Figure 2 Enlarged view of point A in the middle;
[0030] Legend:
[0031] 1. Fuselage; 2. Connecting plate one; 3. Sliding disk; 4. Rotating block; 5. Rotating ball; 6. Sliding shaft one; 7. Connecting block one; 8. Lower sliding column; 9. Connecting column one; 10. Upper sliding column; 11. Motor one; 12. Motor two; 13. Camera; 14. Connecting column two; 15. Support plate; 16. Connecting block two; 17. Rotating plate; 18. Sliding block; 19. Spring; 20. Sliding shaft two; 21. Connecting plate two; 22. Buffer column; 23. Buffer block; 24. Bracket; 25. Wing. Detailed Implementation
[0032] The technical solutions of the present utility model will be clearly and completely described below with reference to the accompanying drawings of the embodiments. Obviously, the described embodiments are only some embodiments of the present utility model, and not all embodiments. Based on the embodiments of the present utility model, all other embodiments obtained by those of ordinary skill in the art without creative effort are within the protection scope of the present utility model.
[0033] Reference Figures 1 to 3 This utility model provides an embodiment of a patrol drone, including a fuselage 1. An adjustment assembly and a buffer assembly are fixedly connected to the outside of the fuselage 1. The adjustment assembly includes a rotating ball 5, and two rotating blocks 4 are fixedly and slidably connected to the outside of the rotating ball 5. The rotating ball 5 provides rotational support to the rotating blocks 4. One of the rotating blocks 4 is fixedly connected to a sliding shaft 6, which drives the rotating block 4 to move. A lower sliding column 8 is slidably connected to the outside of the sliding shaft 6, and an upper sliding column 10 is slidably connected to the outside of the sliding shaft 6. The upper sliding column 10 and the lower sliding column 8 provide sliding space for the sliding shaft 6. The upper sliding column 10 and the lower sliding column 8 are in contact with the outside of the upper sliding column 10. The upper sliding column 10 and the lower sliding column 8 cooperate with each other to realize the angle adjustment of the camera 13. The lower sliding column 8 is fixedly connected to the outside of the motor 12, which drives the lower sliding column 8 to move. The upper sliding column 10 is fixedly connected to the outside of the motor 11, which drives the upper sliding column 10 to move. The motor 11 is fixedly connected to the outside of the connecting plate 11, which provides support for the motor 11. The buffer assembly includes a support plate 15. The support plate 15 is fixedly connected to two connecting blocks 16, which provide support for the connecting blocks 16. The connecting blocks 16 are rotatably connected to a rotating plate 17.
[0034] Connecting block 2 16 provides rotational support for rotating plate 17. A sliding block 18 is rotatably connected to the outside of rotating plate 17, and the sliding block 18 drives rotating plate 17 to move. A sliding shaft 20 is slidably connected to the outside of sliding block 18, and the sliding shaft 20 provides sliding support for sliding block 18. A spring 19 is fixedly connected to the outside of sliding block 18, and the sliding block 18 drives spring 19 to compress. A connecting plate 21 is fixedly connected to the outside of sliding shaft 20, and the connecting plate 21 drives sliding shaft 20 to move. A connecting column 1 9 is fixedly connected to the outside of lower sliding column 8, and an upper sliding column 10 is fixedly connected to the outside of connecting column 1 9. Connecting column 1 9 provides rotational support for lower sliding column 8 and upper sliding column 10. Connecting column 1 9 is fixedly connected to the outside of connecting plate 2, and connecting plate 2 supports connecting column 1 9.
[0035] Reference Figures 2 to 4Another rotating block 4 is externally fixedly connected to a sliding disk 3, which provides sliding space for the rotating block 4. The sliding disk 3 is fixedly connected to the outside of the connecting plate 1 2, which supports the sliding disk 3. The sliding shaft 1 6 is externally fixedly connected to a connecting block 1 7, which drives the connecting block 1 7 to move. The connecting block 1 7 is externally fixedly connected to a camera 13, which drives the camera 13 to move. The connecting plate 2 21 is externally fixedly connected to a buffer column 22, which drives the connecting plate 2 21 to move. The buffer column 22 is externally slidably connected to a connecting column 2 14, which provides sliding space for the buffer column 22. The buffer column 22 is externally fixedly connected to a buffer block 23, which drives the buffer column 22 to move. The buffer block 23 is externally fixedly connected to a bracket 24, which drives the buffer block 23 to move. The fuselage 1 is externally fixedly connected to multiple wings 25, which drive the fuselage 1 to take off. The fuselage 1 is externally fixedly connected to the outside of the connecting plate 1 2, which supports the fuselage 1.
[0036] Working principle: When the product is used, multiple wings 25 on the fuselage 1 are activated, driving the drone to start. After the drone reaches a certain altitude, the camera 13 starts working, and motors 11 and 12 are activated. Motor 11 drives the upper sliding column 10 to move, and motor 12 drives the lower sliding column 8 to move. Both the upper and lower sliding columns 10 and 8 are supported on the connecting plate 2 by the connecting column 9. The sliding shaft 6 is driven by the upper and lower sliding columns 10 and 8, which in turn drives the connecting block 7 to move. The connecting block 7 drives the camera 13 to move, and the connecting block 7 drives the rotating block 4 to rotate on the rotating ball 5. 5. The rotating ball 5 moves on the sliding disk 3, thus enabling the camera 13 to be adjusted to different angles. When the drone is descending, the support 24 lands and drives the buffer block 23 to move. The buffer block 23 drives the buffer column 22 to move. The buffer column 22 drives the connecting plate 21 to move. The connecting plate 21 drives the sliding block 18 to slide on the sliding shaft 20, which compresses the spring 19. The sliding block 18 drives the rotating plate 17 to move. The connecting block 26 provides support for the rotating plate 17. The support plate 15 provides support for the connecting block 26. The connecting column 24 provides support for the support plate 15. Therefore, the drone will not be damaged by the terrain when it lands.
[0037] Finally, it should be noted that the above description is only a preferred embodiment of the present utility model and is not intended to limit the present utility model. Although the present utility model has been described in detail with reference to the foregoing embodiments, those skilled in the art can still modify the technical solutions described in the foregoing embodiments or make equivalent substitutions for some of the technical features. Any modifications, equivalent substitutions, improvements, etc., made within the spirit and principles of the present utility model should be included within the protection scope of the present utility model.
Claims
1. A patrol drone, comprising a fuselage (1), characterized in that: An adjustment assembly is fixedly connected to the outside of the fuselage (1), and a buffer assembly is fixedly connected to the outside of the fuselage (1); The adjustment assembly includes a rotating ball (5), which is fixedly and slidably connected to two rotating blocks (4). One of the rotating blocks (4) is fixedly connected to a sliding shaft (6). The sliding shaft (6) is slidably connected to a lower sliding column (8). The sliding shaft (6) is slidably connected to an upper sliding column (10). The lower sliding column (8) is in contact with the upper sliding column (10). The lower sliding column (8) is fixedly connected to a motor (12). The upper sliding column (10) is fixedly connected to a motor (11). The motor (11) is fixedly connected to a connecting plate (2).
2. The patrol drone according to claim 1, characterized in that: The buffer assembly includes a support plate (15), which is externally fixedly connected to two connecting blocks (16). The connecting blocks (16) are externally rotatably connected to a rotating plate (17). The rotating plate (17) is externally rotatably connected to a sliding block (18). The sliding block (18) is externally slidably connected to a sliding shaft (20). The sliding block (18) is externally fixedly connected to a spring (19). The sliding shaft (20) is externally fixedly connected to a connecting plate (21).
3. The patrol drone according to claim 1, characterized in that: The lower sliding column (8) is fixedly connected to a connecting column one (9), the upper sliding column (10) is fixedly connected to the outside of the connecting column one (9), and the connecting column one (9) is fixedly connected to the outside of the connecting plate one (2).
4. A patrol drone according to claim 1, characterized in that: Another rotating block (4) is externally fixedly connected to a sliding disk (3), which is fixedly connected to the outside of the connecting plate (2).
5. A patrol drone according to claim 1, characterized in that: The sliding shaft (6) is externally fixedly connected to a connecting block (7), and the connecting block (7) is externally fixedly connected to a camera (13).
6. A patrol drone according to claim 2, characterized in that: The connecting plate 2 (21) is fixedly connected to a buffer column (22), and the buffer column (22) is slidably connected to a connecting column 2 (14).
7. A patrol drone according to claim 6, characterized in that: The buffer column (22) is fixedly connected to a buffer block (23), and the buffer block (23) is fixedly connected to a bracket (24).
8. A patrol drone according to claim 1, characterized in that: Multiple wings (25) are fixedly connected to the outside of the fuselage (1), and the fuselage (1) is fixedly connected to the outside of the connecting plate (2).